首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >The Mars Hopper: an impulse-driven,long-range, long-lived mobile platform utilizing in situ Martian resources
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The Mars Hopper: an impulse-driven,long-range, long-lived mobile platform utilizing in situ Martian resources

机译:火星跳跃者:利用原地火星资源的脉冲驱动,远程,长寿命的移动平台

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摘要

The requirements for performance by planetary exploration missions are increasing. Landing at a single location to take data is no longer sufficient. Due to the increasing cost, the missions that provide mobile platforms that can acquire data at displaced locations are becoming more attractive. Landers have also had limited range due to power limitations, limited lifetime of subsystems, and the inability to negotiate rough terrain. The Center for Space Nuclear Research has designed an instrumented platform that can acquire detailed data at hundreds of locations during its lifetime - a Mars Hopper. The Mars Hopper concept utilizes energy from radioisotopic decay in a manner different from any existing radioisotopic power source - as a thermal capacitor. By accumulating the heat from radioisotopic decay for long periods, though, the power of the source can be dramatically increased for short periods. Thus, a radioisotopic thermal rocket is possible. The platform will be able to 'hop' from one location to the next every 2-3 days with a separation of 10-20 km per hop. Each platform will weigh around 50 kg unfuelled which is the condition at deployment. Consequently, several platforms may be deployed on a single launch from Earth. With a lifetime estimated at 10 years, the entire surface of Mars can be mapped in detail by a couple dozen platforms. In addition, hoppers can collect samples and deliver them to the Mars Science Laboratory for more detailed analysis. Furthermore, the basic platform can be deployed to Europa, Titan, and even Venus with alterations - the propulsion system and operations essentially will be the same.
机译:行星勘探任务对性能的要求不断提高。降落在单个位置以获取数据已不再足够。由于成本增加,提供可在流离失所位置获取数据的移动平台的任务变得越来越有吸引力。由于功率限制,子系统的使用寿命有限以及无法协商崎terrain的地形,着陆器的射程也有限。太空核研究中心设计了一个仪器化平台,可以在其生命周期内数百个位置获取详细数据,即火星料斗。 Mars Hopper概念利用放射性同位素衰变产生的能量以不同于任何现有放射性同位素电源的方式-用作热电容器。通过长时间积累放射性同位素衰变产生的热量,可以在短时间内显着增加源的功率。因此,放射性同位素热火箭是可能的。该平台将能够每2-3天从一个位置“跳”到下一个位置,每跳间隔为10-20公里。每个平台未加油的重量约为50公斤,这是部署时的条件。因此,可以在一次地球发射中部署多个平台。估计寿命为10年,火星的整个表面可以通过数十个平台进行详细绘制。此外,料斗可以收集样品并将其送到火星科学实验室进行更详细的分析。此外,该基础平台可以进行更改而部署到欧罗巴,泰坦,甚至金星-推进系统和操作基本上是相同的。

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